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Dynamic Fracture Initiation Toughness of a Gamma (Met-PX) Titanium Aluminide at Elevated Temperatures

机译:高温下γ(Met-PX)铝化钛的动态断裂起始韧性

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摘要

Recently, a new generation of titanium aluminide alloy named Gamma-Met PX (GKSS, Geesthacht, Germany) has been developed with better rolling and postrolling characteristics. Previous work on this alloy has shown the material to have higher strengths at room and elevated temperatures when compared with other gamma titanium aluminides. In particular, this new alloy has shown increased ductility at elevated temperatures under both quasistatic and high-strain-rate uniaxial compressive loading. However, its high-strain-rate tensile ductility at room and elevated temperatures is limited to ~1 pct. In the present article, the results of a study investigating the effects of the loading rate and test temperature on the dynamic fracture initiation toughness in Gamma-Met PX are presented. A modified split Hopkinson pressure bar (MSHPB) was used along with high-speed photography, to determine the dynamic fracture initiation toughness. Three-point-bend fracture tests were conducted at impact speeds in the range 1 to 3.6 m/s and at test temperatures up to 1200 °C. Furthermore, the effect of long-time high-temperature air exposure on the fracture toughness was investigated. The results show that the dynamic fracture initiation toughness decreases at test temperatures beyond 600 °C. Moreover, the dynamic fracture initiation toughness was found to decrease with increasing exposure time. The reasons behind this drop are analyzed and discussed.
机译:最近,已开发出具有更好轧制和轧制后特性的新一代铝化钛合金Gamma-Met PX(GKSS,德国吉萨赫特)。与其他伽马钛铝化物相比,以前对该合金的研究表明该材料在室温和高温下具有更高的强度。尤其是,这种新合金在准静态和高应变速率单轴压缩载荷下均显示出在高温下的延展性。然而,它在室温和高温下的高应变率拉伸延展性被限制在〜1 pct。在本文中,给出了研究负荷率和测试温度对Gamma-Met PX中动态断裂起始韧性的影响的研究结果。修改后的裂合式霍普金森压力棒(MSHPB)与高速摄影技术一起使用,以确定动态断裂起始韧性。在1到3.6 m / s的冲击速度和最高1200°C的测试温度下进行了三点弯曲断裂测试。此外,研究了长时间暴露于高温空气中对断裂韧性的影响。结果表明,在超过600°C的测试温度下,动态断裂起始韧性降低。此外,发现动态断裂起始韧性随着暴露时间的增加而降低。分析和讨论了此下降的原因。

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  • 来源
    《Metallurgical and Materials Transactions A》 |2009年第6期|1400-1412|共13页
  • 作者单位

    Department of Mechanical and Aerospace Engineering Case Western Reserve University Cleveland OH 44106-7222 USA;

    Department of Mechanical and Aerospace Engineering Case Western Reserve University Cleveland OH 44106-7222 USA;

    United States National Aeronautics and Space Administration Glenn Research Center Cleveland OH 44135 USA;

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